US3021463A - Automatic curve sensing system - Google Patents

Automatic curve sensing system Download PDF

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US3021463A
US3021463A US723516A US72351658A US3021463A US 3021463 A US3021463 A US 3021463A US 723516 A US723516 A US 723516A US 72351658 A US72351658 A US 72351658A US 3021463 A US3021463 A US 3021463A
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condenser
curve
sensing
center
sensing system
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Haldemann Heinz
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Rheinmetall Air Defence AG
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Oerlikon Contraves AG
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    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B19/00Programme-control systems
    • G05B19/02Programme-control systems electric
    • G05B19/04Programme control other than numerical control, i.e. in sequence controllers or logic controllers
    • G05B19/12Programme control other than numerical control, i.e. in sequence controllers or logic controllers using record carriers
    • G05B19/122Programme control other than numerical control, i.e. in sequence controllers or logic controllers using record carriers using cards, tapes or discs having conductive paths

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  • the subject of the present invention is a device comprising a carrier for a suitably represented graph curve defining the functional relation between two quantifies, and a sensing device therefor, movable relative to this carrier.
  • Such curve sensing systems form an essential basis for the automatic control of production equipment such as machine tools, apparatus for the manufacture of chemical industrial products, or air conditioning equipment, to
  • the curve representing a given function must first be embodied in a mechanical element, for example in a bent wire or a cam disc, so that the shape of the curve may be mechanically sensed by a feeler.
  • Electro-optical sensing systems have also become known, in which the optical contrast of a graph curve with its environment is used in guiding an electrooptical sensing system having differential photo-electric cells along the curve.
  • Such electro-optical systems give satisfactory results when utilizing transparencies, i.e., films as the carriers of a graph representing a function. It is,
  • FIG. 1 is a diagrammatic sectional elevation of a sensing system, partly shown as an electric block diagram, the section taken along line Y--Y of FIG. 2;
  • FIG. 2 is a section view, of the sensing head, from below, the section being taken along the line II-II of FIG. 1; 7
  • FIG. 3 shows a portion of an arrangement similar to that of FIG. 1, with a layer representing 'a curve and constituting part of a condenser arrangement;
  • FIG. 4 is an illustration analogous to FIG. 2, butshowing a sensing head according to FIG. 3;
  • FIG. 5 is a plan view of a portion of a curve graph with the center A of the sensing head according to FIG. 2 or 4 in an offset position;
  • FIG. 6 is a perspective, partly diagrammatic illustration 2 of a complete sensing device according to the invention
  • FIG. 7 shows the operation of a device according to FIG. 6 in plan view
  • FIG. 8 shows the operation of a device according to FIG. 6 in elevation
  • FIGS. 9, 10 show a simplified device inplan view and elevation, respectively.
  • a sensing head 1 comprises two electrode bodies 11 and 12 of triangular sectiongembedded in an insulating mass 10, arranged symmetrically with respect to the dividing plane S-S (FIG. 2).
  • the sensing device comprises as an essential component a differential condenser arrangement, the electrical field distribution of which is influenced by the layer of material forming the graph curve and constituting part of this condenser arrangement.
  • a differential condenser arrangement the electrical field distribution of which is influenced by the layer of material forming the graph curve and constituting part of this condenser arrangement.
  • ditii'culty special inks can be used for tracing the line, the material of which produces a graph line constituting either a conductive metallic layer (e.g., silver powder inks) or a layer having'an extremely high dielectric constant, so that in both cases the ink layer of the graph sufilciently influences the electric field in the differential condenser arrangement.
  • Thenovel features which are considered as characterelectrode bodies 11, 12 are insulated from one another and are connected to the secondary coil 22 (grounded in the center) of a transformer 20, the primary coil 21 of which is connected to the output of an alternating voltage generator G, so that the lower faces of the two electrodes 11, 12, lying in a common plane, form the layers of a plane condenser, a voltage +Ug. sin wt being applied to one of them, and a voltage -Ug. sin wt, to the other wherein Ug is the maximum absolute value of the amplitude, and ml is the phase angle of the alternating voltage generated in said secondary coil 22.
  • these two triangular condenser layers lies the upper surface of a metal plate 2 as the third layer of'a differential condenser, the plate 2 being connected to ground through a resonance oscillator circuit K.
  • Such a control voltage is adapted to control a tachometrically counter-acting servo-motor drive system comprising an amplifier SV, a motor SM and a tachometer-generator TG driven by the output shaft of the motor SM.
  • the output voltage of this tachometer generator TG is added by an addition member SA to the control voltage 6, and the sum of these voltages, amplified by the amplifier SV is fed as a control voltage a to the motor SM.
  • the insulated carrier ll) of the sensing head 1 has an internal screw thread in mesh with an external screw thread portion 5' of the motor shaft 5 designed as a guide spindle, so that by turning the spindle 5 the sensing head 1 is displaced in a direction Y-Y perpendicular to the plane of symmetry S-S thereof.
  • This displacement takes place at a rate which is the higher, the greater is the error oifset AY of the center A of the sensing head from the center of the layer of the graph, and occurs in that direction which results in a reduction of this offset AY.
  • a graph layer 4 formed as a metallic conductor is connected to one pole of a source of an alternatin voltage G, with the lower face of the sensing head 1 in juxtaposition to it.
  • the sensing head 1' comprises in this embodiment two further layers 13, 14 which are formed likewise symmetrical to the said central plane DD, but are formed trapeziurmshaped asymmetrically to the plane S-S.
  • the layers 11 and 12 as well as the layers 13 and 14 are connected to the ends of one of the centrally grounded transformer coils 23 and 24, respectively, so that in the resonance circuits Ks and K0, respectively, control voltages e and 0' are induced.
  • the control voltage 6 corresponds regarding its positive or negative sign to the direction, and regarding its amplitude to the magnitude of the offset of the graph curve 4 from the center A, while the control voltage 0' indicates by its phase position the positive or negative sign and by its amplitude the magnitude of the angular deviation in between the direction of the graph curve and the direction of the plane S-S. How these control voltages e, a can be evaluated will be explained below with reference to FIG. 6. However, first reference will be had to FIG. 5.
  • a sensing head is represented by its center A and said planes SS and 13-1), and it is assumed that a rotary servo-motor system has turned the sensing head in such a manner, as will be described below, that the central planeiDD extends in a direction perpendicular to the graph curve 4.
  • the angle a indicates the angle between the plane DD of the sensing head and the X-direction.
  • the offset of the center A from the curve 4 in the direction of DD as ascertained by the layers 11 and 12 may have the value R, the components in the X and Y direction of which accordingly have the values, respectively, of:
  • a bar 31 may be shifted to-andfro in its guide 32 by the threaded control spindle 33 of a servo-motor My in the Y-direction of a Cartesian coordinate system.
  • the plate 34 is slidable in the Xdirection of the co-ordinate system, namely by means of the threaded control spindle 35 of the servomotor Mx.
  • the plate 34 is crossed perpendicularly by a rotatable shaft 36, which carries underneath the plate 34 a sensing head 1' according to the FIGS. 3 and 4, and is connected above the plate to a servo-motor Me. as well as to a transformation eight-pole 37, known per so, as an analogue computer element.
  • a servo-motor Me. as well as to a transformation eight-pole 37, known per so, as an analogue computer element.
  • the tachometer generators Ty, Tx, Ta, respectively, and the synchronous transmitters Sy, Sx, Sa, respectively are mounted.
  • From a generator G the three drive systems as well as a voltage divider 38 having a manual adjusting member e.g. hand wheel 39 are supplied with an alternating voltage (for example of a frequency of 400 cycles per second).
  • the graph curve 4 consisting of a conductive layer of a metallic mass situated on the drawing board 40 is connected to this generator, so that for the arrangement of the sensing head 1' with respect to the graph curve 4 the conditions according to FlGS. 3 and 4 prevail.
  • control voltage a is produced by the layers 13 and 14 in the resonance circuit Ka and is supplied to the tachometrically counter-acting servo-motor system comprising the motor Me, the tachometer generator T06 and the amplifier Va, the sensing head being always rotationally or angularly adjusted by the shaft 36 in such a manner that its plane D-D extends perpendicular to the graph curve i (see FIG. 5).
  • a desired tangential velocity is determined by selecting an electrical voltage of desired value which is fed to one input point of the transformation eight-pole" 37;
  • the control voltage 6 is applied (preferably via a pro-amplifier) which is derived from the layers 11, 12 through line b and is obtained by means of a diiferential arrangement in the resonance circuit Ks.
  • the desired control voltage components are formed as follows:
  • FIGS. 7 and 8 corresponds substantially to that according to FIG. 6.
  • the plate 34 is movable in the X direction on guide rods 30 of the bar 31', and the bar 31' itself is movable in the Y direction on stationary guide rods 32.
  • the motors Mx and My each drive through a worm gear device 50x and 50 1, respectively, the shafts 51x and 51y, respectively, which drive twin cord drives 52x and 52y for moving the. components 34 and 31', respectively.
  • FIGS. 9 and 10 corresponds to the FIGS. 1 and 2.
  • Two cord drive pulleys 64 mounted on the shaft 63 are driven by the aid of a servo-motor My and the shaft 63 so that the pull cords 65 driven by the pulley 64 shift the carrier 66 in the Y-direction along the guide rods 67, the sensing head 1 provided with the layers 11 and 12, described with reference to the FIGS. '1 and 2, being mounted on the carrier 66.
  • the plate 2 from which the control voltage for the motor My is derived corresponds to that according to FIG. 1;
  • the operation of the device shown by FIGS. 9 and 10 is analogous to that of the device shown by FIGS. 1 and 2.
  • a source of alternating voltage for electrically sensing the configuration of a given lineal object, particularly of a graph curve ofany shape related to two coordinates and representing the functional relation between two quantities, in combination, a source of alternating voltage; twoplate differential condenser means having a reference center and being connected in circuit with said source; supporting means adapted to carry on one face a lineal object in a'position adjacent to but spaced from and opposite said condenser means, said condenser means ineluding two substantially triangular condenser plates, each being bounded ontwo sides by edges diverging at an angle from said reference center and insulated from each other, said plates being arranged with faces, respectively, in a common plane substantially parallel with said face of said supporting means, and symmetrically with respect to a center plane perpendicular to said common plane and passing through said reference center; a lineal objectrepresenting said graph curve and carried by said supporting means and consisting of a material adapted to cause an unbalance of the electric field of said condenser when
  • said lineal object carried by said supporting means consisting of a material having a particularly high dielectric constant.
  • said supporting means including a carrier member made of noneonductive material and carrying said lineal object, and a support member made of conductive material and located opposite said differential condenser means for being denser means independently of any movement of the latter.
  • said condenser means includes two additional condenser plates arranged in the same plane as said two triangular condenser plates and insulated therefrom and from each other, said additional condenser plates being ar-- ranged within the angular spaces existing between said triangular plates; and bounded on two sides by edges: diverging at an angle from said reference center, said.
  • additional condenser plates being shaped asymmetrical with respect to said center plane, but symmetrical with respect to a second central plane perpendicular both to said center plane and to said common plane, and passing through said reference center, so that the electric field of said two additional condenser plates is unbalanced de pending on, and in proportion to an angle included be tween the direction of said portion of said lineal object, and said second central plane.
  • said differential condenser means including two condenser plates arranged symmetrically with respect to said reference center and connected in opposed phase relation to said source of alternating voltage.

Description

Feb. 13, 1962 H. HALDEMANN 3,021,463
AUTOMATIC CURVE SENSING SYSTEM Filed March 24, 1958 4 Sheets-Sheet 1 Feb. 13, 1962 H. HALDEMANN 3,021,463
AUTOMATIC CURVE SENSING SYSTEM Filed March 24, 1958 4 Sheets-Sheet 2 Q U. l I I wl i 5 N x a; 8 l m I 10 l I u U Q 1 p:-
l M 1 x F X g l I x l X i I l I )y MW:
Feb. 13, 1962 HALDEMANN 3,021,463
AUTOMATIC CURVE SENSING SYSTEM Filed March 24, 1958 4 Sheets-Sheet 3 Feb. 13, 1962 H. HALDEMANN 3,021,463
AUTOMATIC CURVE SENSING SYSTEM Filed March 24, 1958 4 eets-S eet 4 5 I p 37M WNW/v United States Patent 3,021,463 AUTOMATIC CURVE SENSING SYSTEM Heinz Haldemann, Zurich, Switzerland, assignor to Contraves A.G., Zurich, Switzerland Filed Mar. 24, 1958, Ser. No. 723,516 7 Claims priority, application SwitzerlandMar. 22, 1957 14 Claims. (Cl. 318-162) The present invention refers to sensing devices, and more particularly to devices adapted to sense or follow a given graph curve and thereby to furnish data for controlling other devices or their operation.
The subject of the present invention is a device comprising a carrier for a suitably represented graph curve defining the functional relation between two quantifies, and a sensing device therefor, movable relative to this carrier.
Such curve sensing systems form an essential basis for the automatic control of production equipment such as machine tools, apparatus for the manufacture of chemical industrial products, or air conditioning equipment, to
mention only sorneimportant examples. However, such curve sensing systems are used with advantage also for the theoretical analysis of experimentally determined relations betweentwo quantities registered by a graphic recorder, by means of analogue computer machines, for example for the purpose of Fourier analysis or for resolving the two quantities into other components.
It can be readily realized that for a mechanical sensing system the curve representing a given function must first be embodied in a mechanical element, for example in a bent wire or a cam disc, so that the shape of the curve may be mechanically sensed by a feeler.
Electro-optical sensing systems have also become known, in which the optical contrast of a graph curve with its environment is used in guiding an electrooptical sensing system having differential photo-electric cells along the curve. Such electro-optical systems give satisfactory results when utilizing transparencies, i.e., films as the carriers of a graph representing a function. It is,
appended claims. The invention itself, however, both as tovits construction and its method of operation, together with additional objects and advantages thereof, will be best understood from the following description of specific embodiments when read in connection with the accompanying drawings, in which:
FIG. 1 is a diagrammatic sectional elevation of a sensing system, partly shown as an electric block diagram, the section taken along line Y--Y of FIG. 2;
FIG. 2 is a section view, of the sensing head, from below, the section being taken along the line II-II of FIG. 1; 7
FIG. 3 shows a portion of an arrangement similar to that of FIG. 1, with a layer representing 'a curve and constituting part of a condenser arrangement;
FIG. 4 is an illustration analogous to FIG. 2, butshowing a sensing head according to FIG. 3;
FIG. 5 is a plan view of a portion of a curve graph with the center A of the sensing head according to FIG. 2 or 4 in an offset position;
FIG. 6 is a perspective, partly diagrammatic illustration 2 of a complete sensing device according to the invention; FIG. 7 shows the operation of a device according to FIG. 6 in plan view;
FIG. 8 shows the operation of a device according to FIG. 6 in elevation; and
FIGS. 9, 10 show a simplified device inplan view and elevation, respectively.
, According to FIGS. 1 and 2 a sensing head 1 comprises two electrode bodies 11 and 12 of triangular sectiongembedded in an insulating mass 10, arranged symmetrically with respect to the dividing plane S-S (FIG. 2). The
however, highly desirable to be able to sense automation the phenomenon of reflection the difliculty has been encountered that it is not easy to obtain a suiiicient contrast between the reflectivity of the curve drawn with the usual inks or India inks and the reflectivity of the paper base which fact entails the necessity of using comparatively strong light sources or of elaborate circuits for the photo-electric cell current amplifier arrangements. Generally, such electro-optical curve sensing systems are involved, heavy and exposed to the occurrence of breakdowns.
It is therefore a main object of this invention to pro-. vide a sensing device which would be free of the drawbacks of known devices of this kind.
According to the present invention the sensing device comprises as an essential component a differential condenser arrangement, the electrical field distribution of which is influenced by the layer of material forming the graph curve and constituting part of this condenser arrangement. Without ditii'culty special inks can be used for tracing the line, the material of which produces a graph line constituting either a conductive metallic layer (e.g., silver powder inks) or a layer having'an extremely high dielectric constant, so that in both cases the ink layer of the graph sufilciently influences the electric field in the differential condenser arrangement.
Thenovel features which are considered as characterelectrode bodies 11, 12 are insulated from one another and are connected to the secondary coil 22 (grounded in the center) of a transformer 20, the primary coil 21 of which is connected to the output of an alternating voltage generator G, so that the lower faces of the two electrodes 11, 12, lying in a common plane, form the layers of a plane condenser, a voltage +Ug. sin wt being applied to one of them, and a voltage -Ug. sin wt, to the other wherein Ug is the maximum absolute value of the amplitude, and ml is the phase angle of the alternating voltage generated in said secondary coil 22. Opposite these two triangular condenser layers lies the upper surface of a metal plate 2 as the third layer of'a differential condenser, the plate 2 being connected to ground through a resonance oscillator circuit K.
,On the plate 2, i.e. between the lower face of the sensing head 1 and the top surface of said plate 2 a paper strip will have the value zero only when the central axis A of the sensing head 1 intersects the graph layer 4 in the center thereof. However, when this is not the case (see FIGS. v1 and 2) owing to the asymmetrical influence of the layer of the, graph 4 on the field in the'condenser system, a control voltage is. sin wt is generated in the resonance circuit K, the positive or minus sign applying to this voltage, i.e.
.its phase position, depending on the direction of the offset of the graph layer 4 from the center A, while its amplitude i.e. its magnitude, depends on the amount of this deviation.
From FIG. 2 it can be readily seen that the length of that piece of the curve which lies'inthe area of one or the other of the triangular layers 11 or12 increases proportionally-starting from zero, with increasing oifset AY from the center A. For this purpose, the two layers 11, 12- have the shape of triangles, the apices of which almost contact one another in the center A. On account of this, this amplitude e of the control voltage 6 increases with increasing offset AY, while it is practically zero, when the center A of the sensing head is above the center of the graph curve.
Such a control voltage is adapted to control a tachometrically counter-acting servo-motor drive system comprising an amplifier SV, a motor SM and a tachometer-generator TG driven by the output shaft of the motor SM. The output voltage of this tachometer generator TG is added by an addition member SA to the control voltage 6, and the sum of these voltages, amplified by the amplifier SV is fed as a control voltage a to the motor SM.
In accordance with the FIGS. 1 and 2 it is assumed for the sake of simplicity that the insulated carrier ll) of the sensing head 1 has an internal screw thread in mesh with an external screw thread portion 5' of the motor shaft 5 designed as a guide spindle, so that by turning the spindle 5 the sensing head 1 is displaced in a direction Y-Y perpendicular to the plane of symmetry S-S thereof. This displacement takes place at a rate which is the higher, the greater is the error oifset AY of the center A of the sensing head from the center of the layer of the graph, and occurs in that direction which results in a reduction of this offset AY.
Be it assumed that on a paper strip 3 the graph curve 4 representing the function of an abscissa value x in rela tion to an ordinate value y is drawn; when this strip is now moved by any driving means in the direction of the abscissa, i.e. referring to FIG. 1, perpendicular to the plane of the drawing, the sensing head 1 or rather the center A thereof follows automatically the variations of the y-value. Since the instantaneous rotational position of the spindle shaft 5 corresponds under these circumstances to the value of the ordinate y=f(x) associated by the curve with the corresponding value of the abscissa x, there are no difiiculties in evaluating at another place the instantaneous values of the abscissa x as well as the corresponding values of the associated ordinates y, by means of electrical teletransmission systems, either for the purpose of program control or for an analysis of the relation y=f(x) as determined by the graph, by a computer device.
According to the FIGS. 3 and 4 a graph layer 4 formed as a metallic conductor is connected to one pole of a source of an alternatin voltage G, with the lower face of the sensing head 1 in juxtaposition to it. In addition to the two triangular layers ill, 12, the opposed apices of which lie substantially in the center A, and which are formed symmetrical with respect to the dividing plane SS as well as to the central plane DD perpendicular thereto, the sensing head 1' comprises in this embodiment two further layers 13, 14 which are formed likewise symmetrical to the said central plane DD, but are formed trapeziurmshaped asymmetrically to the plane S-S.
According to the FIGS. 3 and 4, the layers 11 and 12 as well as the layers 13 and 14 are connected to the ends of one of the centrally grounded transformer coils 23 and 24, respectively, so that in the resonance circuits Ks and K0, respectively, control voltages e and 0' are induced. Exactly as in the case of the FIGS. 1 and 2, the control voltage 6 corresponds regarding its positive or negative sign to the direction, and regarding its amplitude to the magnitude of the offset of the graph curve 4 from the center A, while the control voltage 0' indicates by its phase position the positive or negative sign and by its amplitude the magnitude of the angular deviation in between the direction of the graph curve and the direction of the plane S-S. How these control voltages e, a can be evaluated will be explained below with reference to FIG. 6. However, first reference will be had to FIG. 5.
The same represents a graph curve 4 in a Cartesian coordinate system X-Y.
In the field contemplated, a sensing head. is represented by its center A and said planes SS and 13-1), and it is assumed that a rotary servo-motor system has turned the sensing head in such a manner, as will be described below, that the central planeiDD extends in a direction perpendicular to the graph curve 4. The angle a then indicates the angle between the plane DD of the sensing head and the X-direction. The offset of the center A from the curve 4 in the direction of DD as ascertained by the layers 11 and 12 may have the value R, the components in the X and Y direction of which accordingly have the values, respectively, of:
Ry:R. sin or Rx=R. cos or On the other hand it is demanded that the center A of the sensing head should follow the graph curve at the tangential velocity V, the components in the the X and Y-directions, respective, have the values:
Vx=V. sin a Vy=-V. cos 0c Accordingly, when the center A of the sensing head is to be moved in the X and Y direction, respectively, by two tachometrically counter-acting drives, the corresponding control components Ay and Ax have to fulfill the following conditions:
Ay=R sin c:-V cos a Ax=R cos a-i-V sin a According to FIG. 6 a bar 31 may be shifted to-andfro in its guide 32 by the threaded control spindle 33 of a servo-motor My in the Y-direction of a Cartesian coordinate system. On the other hand in a guide slot 31 formed in said bar 31 the plate 34 is slidable in the Xdirection of the co-ordinate system, namely by means of the threaded control spindle 35 of the servomotor Mx.
The plate 34 is crossed perpendicularly by a rotatable shaft 36, which carries underneath the plate 34 a sensing head 1' according to the FIGS. 3 and 4, and is connected above the plate to a servo-motor Me. as well as to a transformation eight-pole 37, known per so, as an analogue computer element. On the shafts 33, 35, 36 of the motors My, Mx, Mac the tachometer generators Ty, Tx, Ta, respectively, and the synchronous transmitters Sy, Sx, Sa, respectively, are mounted. From a generator G the three drive systems as well as a voltage divider 38 having a manual adjusting member e.g. hand wheel 39 are supplied with an alternating voltage (for example of a frequency of 400 cycles per second).
Moreover, the graph curve 4 consisting of a conductive layer of a metallic mass situated on the drawing board 40 is connected to this generator, so that for the arrangement of the sensing head 1' with respect to the graph curve 4 the conditions according to FlGS. 3 and 4 prevail.
Through slide contacts, not shown, connections a, and by means of a differential wiring arrangement the control voltage a is produced by the layers 13 and 14 in the resonance circuit Ka and is supplied to the tachometrically counter-acting servo-motor system comprising the motor Me, the tachometer generator T06 and the amplifier Va, the sensing head being always rotationally or angularly adjusted by the shaft 36 in such a manner that its plane D-D extends perpendicular to the graph curve i (see FIG. 5).
By operation of the hand wheel 39 of the voltage divider 33 a desired tangential velocity is determined by selecting an electrical voltage of desired value which is fed to one input point of the transformation eight-pole" 37; To the other input point of this transformation eight-pole the control voltage 6 is applied (preferably via a pro-amplifier) which is derived from the layers 11, 12 through line b and is obtained by means of a diiferential arrangement in the resonance circuit Ks. At the output points of the transformation eight-pole 37 as adjusted angularly by the shaft 36 the desired control voltage components are formed as follows:
AY=V cos u-l-R sin a and AX=+V sin a+R cos a In this manner the center A of the sensing head 1 is caused to follow at a constant tangential velocity V the graph curve 4 situated on the drawing board 40,
and always to assume such a rotational position, that its central plane DD is orientated in adirection perpendicular to the tangent of the graph curve at the particular point. It is then easily possible by the aid of synchronous transmitters Sy, Sx and Sa, respectively, which are mounted on the shafts 33, 35, 36, respectively, to transmit the values of y, x and a to another device, eg to a production machine. In this manner e.g..plates can be out directly and automatically in accordance with the shape drawn as a graph curve 4 on the board 40, by means of a copying oxyacetylene cutter which'is remote-controlled by a device according to FIG. 6. i
The embodiments according to the FIGS. 7 and 8 corresponds substantially to that according to FIG. 6. v
The plate 34 is movable in the X direction on guide rods 30 of the bar 31', and the bar 31' itself is movable in the Y direction on stationary guide rods 32.
The motors Mx and My each drive through a worm gear device 50x and 50 1, respectively, the shafts 51x and 51y, respectively, which drive twin cord drives 52x and 52y for moving the. components 34 and 31', respectively.
The simplified embodiment according to the FIGS. 9 and 10 corresponds to the FIGS. 1 and 2.
By a shaft 61 driven by a motor Mx at constant rotational speed or in dependence of any variable quantity x, a paper strip 40', perforated along the edges, is moved along in the direction of the abscissa X.
Two cord drive pulleys 64 mounted on the shaft 63 are driven by the aid of a servo-motor My and the shaft 63 so that the pull cords 65 driven by the pulley 64 shift the carrier 66 in the Y-direction along the guide rods 67, the sensing head 1 provided with the layers 11 and 12, described with reference to the FIGS. '1 and 2, being mounted on the carrier 66.
The plate 2 from which the control voltage for the motor My is derived, corresponds to that according to FIG. 1; The operation of the device shown by FIGS. 9 and 10 is analogous to that of the device shown by FIGS. 1 and 2.
The principle underlying the various embodiments of devices for capacitatively sensing a graph curve by means of a sensing head acting as a differential condenser may also be used in modified embodiments. For example it may be advantageous to feed the capacitative sensing system with high frequency alternating voltage (100 kilocycles per second), while from the primarily obtained 6 applying current knowledge readily' adapt it for various applications without omitting features that, from the standpoint of prior art, fairly constitute essential characteristics of the generic or specific aspects of this invention and, therefore, such adaptations should and are intended to be comprehended within the meaning and range of equivlance' of the following claims.
What is claimed as new and desired to be secured by Letters Patent is: t,
1. In a sensing system for electrically sensing the configuration of a given lineal object, particularly of a graph curve ofany shape related to two coordinates and representing the functional relation between two quantities, in combination, a source of alternating voltage; twoplate differential condenser means having a reference center and being connected in circuit with said source; supporting means adapted to carry on one face a lineal object in a'position adjacent to but spaced from and opposite said condenser means, said condenser means ineluding two substantially triangular condenser plates, each being bounded ontwo sides by edges diverging at an angle from said reference center and insulated from each other, said plates being arranged with faces, respectively, in a common plane substantially parallel with said face of said supporting means, and symmetrically with respect to a center plane perpendicular to said common plane and passing through said reference center; a lineal objectrepresenting said graph curve and carried by said supporting means and consisting of a material adapted to cause an unbalance of the electric field of said condenser when at least that portion of said lineal object which is located opposite said condenser is'in a position other than substantially in alignment with said reference center; moving means for moving said condenser means and said supporting means carrying said lineal object, relative to one another; and electrical control means operatively connected between said condenser means and said moving means for controlling the latter depending upon said unbalance so as to operate said moving means in a manner causing said portion of said lineal object to assume a position substantially in alignment with said reference center.
2. A sensing system as claimed in claim 1, said supporting means being substantially madeof a material having a predetermined degree of electric conductivity including zero conductivity, and said lineal object carried by said supporting means consisting of a material having a conductivity sufficiently different from that of said supporting means to make it adapted to cause an unbalance of the electric field of said condenser when at least that portion of said lineal objectwhich is located opposite said condenser is in a position other than substantially control voltages control signals of lower frequency for the servo-motors may be derived. 7
It will be understood that each of the elements described above, or two or more together, may also find a useful application in other types of sensing devices differing from the types described above.
While the invention has been illustrated and described as embodied in sensing devices for securing a given curve, it is not intended to be limited to the details shown, since various modifications and structural changes may be made without departing in any way from the spirit of the present invention.
Without further analysis, the foregoing will so fully reveal the gist of the present invention that others can by p in alignment with said reference center.
3. A sensing system as claimed in claim 1, said lineal object carried by said supporting means consisting of an electrically conductive material.
4. A sensing system as claimed in claim 1, said lineal object carried by said supporting means consisting of a material having a particularly high dielectric constant.
5. A sensing system as set forth in claim 1, said supporting means being non-conductive and said lineal object being made ofconductive material and conductive 1y connected to said source of alternating voltage, and inductance means connected with said condenser means to form therewith differential oscillator means capable of producing a control voltage for operating said moving means.
6. A sensing system as set forth in claim 1, said supporting means including a carrier member made of noneonductive material and carrying said lineal object, and a support member made of conductive material and located opposite said differential condenser means for being denser means independently of any movement of the latter.
7. A sensing system as set forth in claim 1, wherein said condenser means includes two additional condenser plates arranged in the same plane as said two triangular condenser plates and insulated therefrom and from each other, said additional condenser plates being ar-- ranged within the angular spaces existing between said triangular plates; and bounded on two sides by edges: diverging at an angle from said reference center, said. additional condenser plates being shaped asymmetrical with respect to said center plane, but symmetrical with respect to a second central plane perpendicular both to said center plane and to said common plane, and passing through said reference center, so that the electric field of said two additional condenser plates is unbalanced de pending on, and in proportion to an angle included be tween the direction of said portion of said lineal object, and said second central plane.
8. A sensing system as set foith in claim 6, wherein: said lineal object is a graph curve related to two coordinates, said carrier member being movable in the direction of one of said coordinates, while said dififerential condenser means is movable by said moving means, in the direction of the other one of said coordinates; and wherein said control means include circuit means connected in series between said conductive support member and said moving means, and being capable of translating an alternating voltage applied thereto by, said source via said condenser means into a control voltage for controlling said moving means, said control voltage depending upon the degree and direction of the o=ut-o-f-alignment position of said reference center with respect to the center of said lineal object at the particular moment.
9. A sensing system as set forth in claim 8, said differential condenser means including two condenser plates arranged symmetrically with respect to said reference center and connected in opposed phase relation to said source of alternating voltage.
10. A sensing system as set forth in claim 5, said lineal object being a graph curve related to two predetermined coordinates, and said supporting means being stationary, said differential condenser means being movable independently in either one of the directions of said two coordinates, and said moving means being arranged to effect the movement in one of said coordinate directions under the action of said control means.
11. A sensing system as set forth in claim 10, said oscillator means being capable of producing a control voltage depending in its phase position on the direction, and in its magnitude on the degree, of the out-of-alignmerit position of said reference center with respect to the center of said lineal object whenever such out-of-alignmerit position occurs.
12. A sensing system as set forth in claim 7, including first inductance means connected with said two triangular condenser plates to form therewith first diflierential oscillator means, and second inductance means connected with said additional condenser plates to form therewith second difierential oscillator means, said first osc'llator means being capable of producing a first control voltage depending in its phase position on the direction, and in its magnitude on the degree, of the outof-alignment position of said reference center with respect to the center of said lineal object of the particular moment, and said second oscillator means being capable of producing a second control voltage depending, in its phase position, on the direction, and in its magnitude, on the amount of said angle included between the direction of said portion of said linear object and said second central plane, said oscillator means being connected with said control means for applying there-to said control voltages so as to actuate said control means.
13. A sensing system as set forth in claim 12, including second moving means for turning said differential condenser means about an axis perpendicular to said common plane, said control means including circuit means for applying said second control voltage to said second moving means.
14. A sensing system as set forth in claim 13, including a component resolver means having two input terminals, one of which is connected to said first oscillator means, and serving as a trigonometrical analogue computer member, said member being mounted for turning movement jointly with said diiferential condenser means so as to assume at all times an angular position about said axis substantially identical with said angle included between the direction of said portion of said lineal object and said second central plane, said member further having two output terminals connected to said first and second control means, respectively; voltage control means in circuit between said source of alternating voltage and said computer member for deriving from said alternating voltage a third control voltage and for adjusting the velocity of said differential condenser means along said linear object by applying said third control voltage to one of said input terminals, said member being capable of wnverting said third control voltage and said first control voltage derived from said two triangular condenser plates through said first oscillator means into corresponding control components and of delivering the same via said output terminals to said control means for causing said moving means to move said differential condenser means in the direction of said coordinates, respectively.
References Cited in the file of this patent UNITED STATES PATENTS 2,590,091 Devol Mar. 25, 1952 2,611,115 Johnston Sept. 16, 1952 2,679,620 Berry May 25, 1954 2,721,989 Gates Oct. 25, 1955 2,835,858 ivios-eley May 20, 1958
US723516A 1957-03-22 1958-03-24 Automatic curve sensing system Expired - Lifetime US3021463A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3207964A (en) * 1962-01-31 1965-09-21 Atlantic Refining Co Automatic curve following system
US3215914A (en) * 1962-08-28 1965-11-02 William E Patterson Fast and slow dual photo-cell bridge plural servo-motor control for duplicating machines
US3548173A (en) * 1966-09-08 1970-12-15 Ford Motor Co Numerically controlled surface development method for preparing body contours
US3787726A (en) * 1970-10-23 1974-01-22 W Krapp Conductive line following device for steering a vehicle

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2590091A (en) * 1946-04-03 1952-03-25 Remington Rand Inc Magnetic process control
US2611115A (en) * 1945-10-26 1952-09-16 Lawrence H Johnston Automatic curve follower
US2679620A (en) * 1952-04-30 1954-05-25 Gen Electric Line follower
US2721989A (en) * 1949-11-29 1955-10-25 United Shoe Machinery Corp Recording magnitudes in ratio form
US2835858A (en) * 1955-05-24 1958-05-20 F L Moseley Company Curve or line follower apparatus

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2611115A (en) * 1945-10-26 1952-09-16 Lawrence H Johnston Automatic curve follower
US2590091A (en) * 1946-04-03 1952-03-25 Remington Rand Inc Magnetic process control
US2721989A (en) * 1949-11-29 1955-10-25 United Shoe Machinery Corp Recording magnitudes in ratio form
US2679620A (en) * 1952-04-30 1954-05-25 Gen Electric Line follower
US2835858A (en) * 1955-05-24 1958-05-20 F L Moseley Company Curve or line follower apparatus

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3207964A (en) * 1962-01-31 1965-09-21 Atlantic Refining Co Automatic curve following system
US3215914A (en) * 1962-08-28 1965-11-02 William E Patterson Fast and slow dual photo-cell bridge plural servo-motor control for duplicating machines
US3548173A (en) * 1966-09-08 1970-12-15 Ford Motor Co Numerically controlled surface development method for preparing body contours
US3787726A (en) * 1970-10-23 1974-01-22 W Krapp Conductive line following device for steering a vehicle

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